ADAPTOR AND PAYLOAD-LAUNCHING ROCKET

摘要

The purpose of the present invention is to provide: an adaptor which can, using a simple configuration, reduce vibration inputted in a payload; and a payload-launching rocket. This adaptor (1) reduces the vibration of a payload contained in a payload-launching rocket and is provided between the payload and the rocket section. The adaptor (1) is provided with: a tube member having a double structure and comprising an outer tube (11) and an inner tube (12); a first elastic member (21) joined at one end of the tube member to the outer tube (11) and to the inner tube (12); and a second elastic member (22) joined at the other end of the tube member to the outer tube and to the inner tube. The adaptor (1) is connected to the payload on the inner tube side or the outer tube side of the one end of the tube member and is connected to the front end of the rocket section on the outer tube side or the inner tube side of the other end of the tube member.